Journal
COMBUSTION EXPLOSION AND SHOCK WAVES
Volume 46, Issue 3, Pages 315-324Publisher
CONSULTANTS BUREAU/SPRINGER
DOI: 10.1007/s10573-010-0044-2
Keywords
solid propellant; coolant; modeling; two-zone burning
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A mathematical model for combustion of a propellant with a coolant taking into account the two-zone structure of the combustion front due to condensed- and gas-phase reactions was developed and examined. Formulas for the burning rate, reaction-zone temperature, and burning-rate sensitivity to internal and external parameters of the system were derived in analytical form. The burning rate was examined numerically as a function of pressure, the characteristic size of the system, component content, and thermodynamic and kinetic parameters. Recommendations are given on methods of obtaining particular ballistic properties by varying the initial parameters of the system.
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